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561.
Y.S. Ge C.T. RussellT.-S. Hsu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(8):1243-1251
In 2001, 2002 and 2003, the Polar spacecraft probed the near equatorial plasma sheet at 9 RE near local midnight. Using the magnetic field observations, the signatures at substorm onsets are studied. Close to the flux pile-up region, the Polar spacecraft readily detects the dipolarization front, especially for pseudo onsets. An event with two distinct onsets has been examined. The signatures are found to be consistent with the multiple-onset model suggested by Russell [Russell, C.T. How northward turnings of the IMF can lead to substorm expansion onsets. Geophys. Res. Lett. 27, 3257–3259, 2000] which is a modified Near-Earth Neutral Line (NENL) model. Another similar event is also examined showing the effects of different Interplanetary Magnetic Field (IMF) conditions upon substorms. Moreover, ground effects can be very weak compared to in situ observations, especially for pseudo onsets, because these signatures appear to be localized and not global. 相似文献
562.
563.
M.C. Rabello-Soares Sylvain G. Korzennik J. Schou 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(6):861-867
Using full-disk observations obtained with the Michelson Doppler Imager (MDI) on board the Solar and Heliospheric Observatory (SOHO) spacecraft, we present variations of the solar acoustic mode frequencies caused by the solar activity cycle. High-degree (100 < ? < 900) solar acoustic modes were analyzed using global helioseismology analysis techniques over most of solar cycle 23. We followed the methodology described in details in [Korzennik, S.G., Rabello-Soares, M.C., Schou, J. On the determination of Michelson Doppler Imager high-degree mode frequencies. ApJ 602, 481–515, 2004] to infer unbiased estimates of high-degree mode parameters ([see also Rabello-Soares, M.C., Korzennik, S.G., Schou, J. High-degree mode frequencies: changes with solar cycle. ESA SP-624, 2006]). We have removed most of the known instrumental and observational effects that affect specifically high-degree modes. We show that the high-degree changes are in good agreement with the medium-degree results, except for years when the instrument was highly defocused. We analyzed and discuss the effect of defocusing on high-degree estimation. Our results for high-degree modes confirm that the frequency shift scaled by the relative mode inertia is a function of frequency and it is independent of degree. 相似文献
564.
C. de Jager A. Ollongren Tj. de Graaf B. J. Levin M. Tucker 《Space Science Reviews》1969,9(5):740-742
565.
ARTEMIS Mission Design 总被引:2,自引:0,他引:2
Theodore H. Sweetser Stephen B. Broschart Vassilis Angelopoulos Gregory J. Whiffen David C. Folta Min-Kun Chung Sara J. Hatch Mark A. Woodard 《Space Science Reviews》2011,165(1-4):27-57
The ARTEMIS mission takes two of the five THEMIS spacecraft beyond their prime mission objectives and reuses them to study the Moon and the lunar space environment. Although the spacecraft and fuel resources were tailored to space observations from Earth orbit, sufficient fuel margins, spacecraft capability, and operational flexibility were present that with a circuitous, ballistic, constrained-thrust trajectory, new scientific information could be gleaned from the instruments near the Moon and in lunar orbit. We discuss the challenges of ARTEMIS trajectory design and describe its current implementation to address both heliophysics and planetary science objectives. In particular, we explain the challenges imposed by the constraints of the orbiting hardware and describe the trajectory solutions found in prolonged ballistic flight paths that include multiple lunar approaches, lunar flybys, low-energy trajectory segments, lunar Lissajous orbits, and low-lunar-periapse orbits. We conclude with a discussion of the risks that we took to enable the development and implementation of ARTEMIS. 相似文献
566.
E. A. Botan 《Space Science Reviews》1964,3(5-6):715-723
567.
Sanneman Richard W. Gupta Someshwar C. 《IEEE transactions on aerospace and electronic systems》1966,(5):570-581
Pontryagin's maximum principle is applied to minimize the time for a phase-locked loop to lock to a step change in frequency. In particular, a Type II phase-locked loop is considered in detail. Phase control and frequency control of the input signal are analyzed with the nonlinearity of the phase detector taken into consideration. It is shown that application of Pontryagin's maximum principle offers a decided advantage in shortening this time by proper control. 相似文献
568.
Two new methods of landmark navigation were recently presented. The landmarks are assumed to be within sight of the navigator but with unknown positions. Both methods require computations which are time consuming when a computer is not available. This correspondence presents the concept of a new navigation device called ?landmark navigation rule? which eliminates all the computation effort required in both new methods. The device is simple in construction, lightweight, and consumes no power. 相似文献
569.
570.
This contribution describes the formation of circumstellar disks and their earliest evolutionary phases when self-gravity
in the disk plays a crucial role in eliciting the transport of mass and angular momentum. We first discuss the formation of
protostellar disks within the context of analytic infall-collapse solutions. We then discuss our efforts to understand the
behavior of the newly formed disks. Our specific approach consists of performing a detailed analysis of a simplified model
disk which is susceptible to the growth of a spiral instability. Using a combination of numerical simulation and semi-analytic
analysis, we show how the dramatic early phase of mass and angular momentum transport in the disk can be explained by a second-order
nonlinear process involving self-interaction of a dominant two-armed spiral mode.
This revised version was published online in June 2006 with corrections to the Cover Date. 相似文献